View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 58390U 26144.99140809 +.00000000 +00000-0 +13396-3 0 00000
2 58390 53.1604 5.9460 0000668 71.0594 289.0481 15.34370536 05
| Epoch (UTC): | 24 May 2026 23:47:37 |
| Eccentricity: | 0.0000668 |
| inclination: | 53.1604° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 5.9460° |
| argument of perigee: | 71.0594° |
| revolutions per day: | 15.34370536 |
| mean anomaly at epoch: | 289.0481° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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